STC SR09263RC-D

FAA Form 8110-2 (5/14) Page 1 of 3

Number: SR09263RC-D

Part 27 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: R0001RD Make: Airbus Helicopters Model: EC120B Description of Type Design Change:

The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Date of Application: February 22, 2001 Date Reissued: 08/01/03; 12/06/04; 11/01/16 Date of Issuance: October 15, 2001 Date Amended: May 08, 2009; February 09, 2011

Signature

Title James A. Grigg Acting Manager, Fort Worth Aircraft Certification Office, Southwest Region Safran Electronics & Defense, Avionics USA, LLC 2802 Safran Drive Grand Prairie, TX 75052

FAA Form 8110-2 (5/14) Page 2 of 3

Transfer the ownership of Supplemental Type Certificate Number: SR09263RC-D

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR09263RC-D

FAA Form 8110-2 (5/14) Page 3 of 3

Date of Issuance: October 15, 2001 Date Amended: February 9, 2011 Date of Reissuance: November 1, 2016

Description of Type Design Change (Continued):

1. Installation of a SFIM VFR Autopilot System in accordance with AEC Drawing List 120A82-8010, Revision E, dated June 2, 2006, or later FAA approved revision. Rotorcraft Flight Manual Supplement (RFMS) 120FMS-012, Revision B, dated April 7, 2006, or later FAA approved revision is required. Instructions for Continued Airworthiness (ICA) PA85-120MMS-001, Revision B, June 6, 2002, or later accepted revision is required.

2. Installation of a SAGEM VFR Autopilot System coupled with a SAGEM ICDS-8A Integrated Cockpit Display System (ICDS), per STC SR09450RC, in accordance with SAGEM Master Drawing List 120-0001, Revision D, dated April 1, 2009, or later FAA approved revision. This configuration is further defined as the -01 configuration in SAGEM Installation Drawing 120-1002-01, Revision C, dated March 30, 2009, or later FAA approved revision.

Rotorcraft Flight Manual Supplement (RFMS) 120FMS-012, Revision C, dated May 11, 2009, or later FAA approved revision is required. Instructions for Continued Airworthiness (ICA) SA-08R-E-005, Revision --, dated February 20, 2009, or later accepted revision is required. NOTE: This configuration is not available after February 9, 2011.

3. Installation of a SAGEM VFR Autopilot System coupled with a SAGEM ICDS-8A Integrated Cockpit Display System (ICDS), per STC SR09450RC, in accordance with SAGEM Master Drawing List 120-0001, Revision D, dated April 1, 2009, or later FAA approved revision. This configuration is further defined as the -02 configuration in SAGEM Installation Drawing 120-1002-02, Revision C, dated March 30, 2009, or later FAA approved revision.

Rotorcraft Flight Manual Supplement (RFMS) 120FMS-012, Revision C, dated May 11, 2009, or later FAA approved revision is required. Instructions for Continued Airworthiness (ICA) SA-08R-E-005, Revision --, February 20, 2009, or later accepted revision is required. NOTE: This configuration is not available after February 9, 2011.

4. Installation of a SAGEM VFR Autopilot System coupled with a SAGEM ICDS-8A Integrated Cockpit Display System (ICDS), per STC SR09450RC, in accordance with SAGEM Master Drawing List 120-0001, Revision F, dated August 6, 2010, or later FAA approved revision. This configuration is further defined as the -03 configuration in SAGEM Installation Drawing 120-1002, Revision D, dated July 10, 2010, or later FAA approved revision.

Rotorcraft Flight Manual Supplement (RFMS) 120FMS-012, Revision C, dated May 11, 2009, or later FAA approved revision is required. Instructions for Continued Airworthiness (ICA) SA-08R-E-005, Revision A, dated September 27, 2010, or later accepted revision is required.

5. Installation of a SAGEM VFR Autopilot System coupled with a SAGEM ICDS-8A Integrated Cockpit Display System (ICDS), per STC SR09450RC, in accordance with SAGEM Master Drawing List 120-0001, Revision F, dated August 6, 2010, or later FAA approved revision. This configuration is further defined as the -04 configuration in SAGEM Installation Drawing 120-1002, Revision D, dated July 10, 2010, or later FAA approved revision.

Rotorcraft Flight Manual Supplement (RFMS) 120FMS-012, Revision C, dated May 11, 2009, or later FAA approved revision is required. Instructions for Continued Airworthiness (ICA) SA-08R-E-005, Revision A, September 27, 2010, or later accepted revision is required.

-END-

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR09263RC-D

FAA Form 8110-2 (5/14) Page 4 of 3